YAOGAN 30, 41473
Orbit data source: Space-Track
YAOGAN 30, 41473 is a payload satellite owned by PLA SSF (CN) in SSO that was launched on Sun, 15 May 2016 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41473 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Defense Imaging
Bus & Motor
CAST-2000?, Unknown motor
Mass
800 kg wet, 800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
5.141 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 YAOGAN 30
1 41473U 16029A 26297.34248059 .00000161 00000-0 30461-4 0 9994
2 41473 97.8870 344.3333 0015827 169.7042 190.4495 14.76273905562723Epoch: 2026-10-24T08:13Z
TLE epoch observation values (Epoch: 2026-10-24T08:13:10.322Z)
Latitude
-0.00007°
Longitude
-171.70974°
Altitude
655.055 km
Speed
7.524 km/s
True Right ascension
22h 57m 19s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.26 km
Perigee altitude
627.051 km
Semi-major axis
7,016.293 km
Eccentricity
0.00158
Inclination
97.887°
RAAN
344.3333°
Arg. of periapsis
169.7042°
True anomaly
190.41667°
Mean anomaly
190.4495°
Eccentric anomaly
190.43308°
Mean motion
3.69302 °/min
Orbital period
97.48 mins
BSTAR
0.000030461
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Other satellites on launch #29 in the year 2016 (2016-05-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.YAOGAN 30 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-25 02:16:21.164Z | 104.643° ESE | 2026-10-25 02:18:21.164Z | 73.574° E | 20.129° | 2026-10-25 02:21:21.164Z | 25.762° NE |
| 6 mins | 2026-10-25 03:52:21.164Z | 205.647° SW | 2026-10-25 03:55:21.164Z | 273.898° WNW | 36.218° | 2026-10-25 03:58:21.164Z | 325.304° NNW |
| 6 mins | 2026-10-25 15:43:21.164Z | 38.663° NE | 2026-10-25 15:45:21.164Z | 83.204° E | 42.374° | 2026-10-25 15:49:21.164Z | 168.514° S |
| 4 mins | 2026-10-25 17:20:21.164Z | 319.551° NNW | 2026-10-25 17:22:21.164Z | 287.222° WNW | 16.651° | 2026-10-25 17:24:21.164Z | 258.568° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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